EP 1069281 B1 20050727 - Pre-stressed/pre-compressed gas turbine nozzle
Title (en)
Pre-stressed/pre-compressed gas turbine nozzle
Title (de)
Vorgespannte Gasturbinenleitschaufel
Title (fr)
Aube de guidage sous prétension pour turbine à gaz
Publication
Application
Priority
US 35433699 A 19990716
Abstract (en)
[origin: EP1069281A2] A method of increasing low cycle fatigue life of a turbine nozzle (10) comprising a plurality of stationary airfoils (12) extending between radially inner and outer ring segments (16, 14) comprising a) providing at least one radial passage (22) in each of the plurality of airfoils; b) installing a rod in the radial passage extending between the radially inner and outer ring segments and fixing one end of the rod to one of the inner and outer rings; and c) preloading the rod (56) to compress the airfoil between the inner and outer ring segments. <IMAGE>
IPC 1-7
IPC 8 full level
F01D 9/02 (2006.01); F01D 5/14 (2006.01); F01D 5/18 (2006.01)
CPC (source: EP KR US)
F01D 5/147 (2013.01 - EP US); F01D 5/189 (2013.01 - EP US); F01D 9/02 (2013.01 - KR); F05D 2240/10 (2013.01 - EP US); F05D 2240/81 (2013.01 - EP US); F05D 2260/205 (2013.01 - EP US); F05D 2260/2322 (2013.01 - EP US); Y10T 29/49323 (2015.01 - EP US)
Designated contracting state (EPC)
AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE
DOCDB simple family (publication)
EP 1069281 A2 20010117; EP 1069281 A3 20021211; EP 1069281 B1 20050727; AT E300664 T1 20050815; DE 60021487 D1 20050901; DE 60021487 T2 20060518; JP 2001041003 A 20010213; JP 4738567 B2 20110803; KR 20010014988 A 20010226; US 2001018019 A1 20010830; US 6402463 B2 20020611
DOCDB simple family (application)
EP 00304399 A 20000524; AT 00304399 T 20000524; DE 60021487 T 20000524; JP 2000174587 A 20000612; KR 20000029915 A 20000601; US 77803301 A 20010207